GB1417614A - Power plant - Google Patents
Power plantInfo
- Publication number
- GB1417614A GB1417614A GB1475473A GB1475473A GB1417614A GB 1417614 A GB1417614 A GB 1417614A GB 1475473 A GB1475473 A GB 1475473A GB 1475473 A GB1475473 A GB 1475473A GB 1417614 A GB1417614 A GB 1417614A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hydrogen peroxide
- valves
- motor
- gas turbine
- fuel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 abstract 10
- 239000000446 fuel Substances 0.000 abstract 4
- 239000007789 gas Substances 0.000 abstract 4
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 238000000354 decomposition reaction Methods 0.000 abstract 2
- 230000001133 acceleration Effects 0.000 abstract 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract 1
- 230000005540 biological transmission Effects 0.000 abstract 1
- 239000003054 catalyst Substances 0.000 abstract 1
- 238000003421 catalytic decomposition reaction Methods 0.000 abstract 1
- 238000001816 cooling Methods 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 239000001301 oxygen Substances 0.000 abstract 1
- 229910052760 oxygen Inorganic materials 0.000 abstract 1
- 238000013022 venting Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
1417614 Gas turbine engines NISSAN MOTOR CO Ltd 27 March 1973 [1 April 1972 25 April 1972] 14754/73 Heading FIG A gas turbine engine comprises a casing 14 internally divided by a catalyst 22 to form a feed chamber receiving hydrogen peroxide, and a combustion chamber 20 into which the steam and oxygen formed by exothermic catalytic decomposition of the hydrogen peroxide is fed to combust with liquid fuel 32 fed via a nozzle 34a, the combustion products then being directed against the blading 52 of the turbine. As shown, the combustion products pass through a Venturi portion 48 into flow passages 50, and cooling air is drawn into the hot gases through an inlet 56 in the Venturi portion. Turbines 30, 42 driven by the decomposition products of the hydrogen peroxide drive pumps 24, 36 feeding the hydrogen peroxide and fuel respectively. Valves 16, 46 controlling the supply of hydrogen peroxide and the venting of the decomposition products respectively, are themselves controlled in response to torque demand. Again, Fig. 2 (not shown), the air nozzle 56 and fuel pump 36 together with its associated parts are omitted, and a throttle valve (66) controls the fuel feed. Also, an energy storing flywheel (70) is coupled to the engine through a centrifugal clutch (74). A speed sensor on the flywheel shaft controls valves 16 and (66) to close the valves when the speed exceeds a predetermined value. The flywheel drives a vehicle multi-speed transmission (88) through a fluid coupling (86). In Fig. 3 (not shown), the flywheel shaft drives an electric generator (98) connected to an electric motor (104) driving the vehicle wheels. A battery (108) is connected to the motor and the generator to store excess electrical energy and to provide additional energy for the motor during vehicle acceleration. The gas turbine engine may alternatively be utilized in driving ships, aircraft, external electrical generators, emergency electrical power sources and/or portable electrical generators.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3280872A JPS4899509A (en) | 1972-04-01 | 1972-04-01 | |
JP4166972A JPS491926A (en) | 1972-04-25 | 1972-04-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1417614A true GB1417614A (en) | 1975-12-10 |
Family
ID=26371390
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1475473A Expired GB1417614A (en) | 1972-04-01 | 1973-03-27 | Power plant |
Country Status (3)
Country | Link |
---|---|
US (1) | US3898794A (en) |
FR (1) | FR2179019B1 (en) |
GB (1) | GB1417614A (en) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS51145504A (en) * | 1975-05-28 | 1976-12-14 | Nissan Motor Co Ltd | A reformer |
US4047380A (en) * | 1976-04-09 | 1977-09-13 | The United States Of America As Represented By The Secretary Of The Navy | Combustion system using dilute hydrogen peroxide |
US4135361A (en) * | 1976-10-26 | 1979-01-23 | The Charles Stark Draper Laboratory, Inc. | Self-contained heat generating system |
EP0144094B1 (en) * | 1983-12-07 | 1988-10-19 | Kabushiki Kaisha Toshiba | Nitrogen oxides decreasing combustion method |
US4759178A (en) * | 1987-03-17 | 1988-07-26 | Williams International Corporation | Aircraft auxiliary power unit |
JP2759748B2 (en) * | 1993-11-20 | 1998-05-28 | 川崎重工業株式会社 | High temperature and high pressure gas generator for turbine drive |
FR2728627B1 (en) * | 1994-12-27 | 1997-03-14 | Europ Propulsion | TANK SELF-PRESSURIZATION |
US6255009B1 (en) * | 1998-03-28 | 2001-07-03 | The United States Of America As Represented By The Secretary Of The Navy | Combined cycle power generation using controlled hydrogen peroxide decomposition |
FR2792060B1 (en) * | 1999-04-06 | 2001-09-07 | Air Jonction Tech | PROCESS FOR PRODUCING STEAM FROM SUPERHEATED WATER, STEAM GENERATOR USING THE SAME AND ITS INDUSTRIAL APPLICATIONS |
GB9917404D0 (en) * | 1999-07-26 | 2000-08-23 | Secr Defence | Hydrogen peroxide based propulsion system |
US6349787B1 (en) * | 2000-05-08 | 2002-02-26 | Farouk Dakhil | Vehicle having a turbine engine and a flywheel powered by liquid nitrogen |
US6661112B2 (en) * | 2001-04-02 | 2003-12-09 | Bravo Zulu International | Fluid control system with automatic recovery feature |
US6532741B2 (en) * | 2001-06-29 | 2003-03-18 | United Technologies Corporation | Gas generator for producing adjustable flow |
CN1659372B (en) | 2002-04-11 | 2012-12-26 | 克尼尔维利科技有限公司 | Water combustion technology-methods, processes, systems and apparatus for the combustion of hydrogen and oxygen |
US20050066662A1 (en) * | 2003-09-26 | 2005-03-31 | Cronce Donald T. | Using solids as peroxide source for fuel cell applications, process and product thereof |
US20060174605A1 (en) * | 2005-02-07 | 2006-08-10 | Berry Benny L | Berry zero hydrocarbons engine |
US20070107433A1 (en) * | 2005-11-15 | 2007-05-17 | Berry Benny L | Hybrid electric steam turbine automotive engine |
US7966805B2 (en) * | 2007-05-15 | 2011-06-28 | Raytheon Company | Hydroxyl amine based staged combustion hybrid rocket motor |
US8205827B2 (en) * | 2008-01-23 | 2012-06-26 | Aurora Flight Sciences Corporation | Hydrazine monopropellant decomposition air turboprop engine |
EP2508498A1 (en) * | 2011-04-09 | 2012-10-10 | Eckhard Braun | Solar fuel based on monergol hydrogen peroxide |
US20120282558A1 (en) * | 2011-05-05 | 2012-11-08 | General Electric Company | Combustor nozzle and method for supplying fuel to a combustor |
RU2527010C2 (en) * | 2012-08-24 | 2014-08-27 | Федеральное государственное бюджетное учреждение науки Институт энергетических проблем химической физики Российской академии наук | Gas turbine plant with water steam injection |
RU2527007C2 (en) * | 2012-08-24 | 2014-08-27 | Федеральное государственное бюджетное учреждение науки Институт энергетических проблем химической физики Российской академии наук | Gas turbine plant with supply of steam-fuel mixture |
EA202091967A1 (en) | 2014-08-15 | 2021-03-31 | Глоубал Ойл Эор Системз, Лтд. | HYDROGEN PEROXIDE STEAM GENERATOR FOR OIL FIELD APPLICATIONS |
CN106704531A (en) * | 2015-11-16 | 2017-05-24 | 熵零股份有限公司 | Energy adjusting method |
CN105841193B (en) | 2016-05-18 | 2018-07-20 | 葛明龙 | Two kinds of aerospace fanjets |
DE102019001876B3 (en) | 2019-03-15 | 2020-06-10 | Tivadar Menyhart | Method, device and system for operating internal combustion engines with a significantly increased pressure ratio and vehicle with this system |
WO2021239186A1 (en) * | 2020-05-25 | 2021-12-02 | Nexth202 Gmbh Zwickau | Steam-operated turbine system |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2450950A (en) * | 1945-06-11 | 1948-10-12 | Daniel And Florence Guggenheim | Gas blast actuated auxiliary turbine for gas blast propelled craft |
US2926492A (en) * | 1951-01-17 | 1960-03-01 | Bendix Aviat Corp | Self contained power plant using liquid decomposed into gaseous products |
GB763015A (en) * | 1954-05-25 | 1956-12-05 | Napier & Son Ltd | Power gas producing apparatus especially for rocket type propulsion devices |
US3229462A (en) * | 1964-04-22 | 1966-01-18 | Fatica Nicholas | Propulsion system |
US3581504A (en) * | 1968-08-28 | 1971-06-01 | Aerojet General Co | Monopropellant turbo gas generator |
US3740945A (en) * | 1969-02-27 | 1973-06-26 | Thiokol Chemical Corp | Injector for rocket motors using high viscosity fuel |
-
1973
- 1973-03-26 US US344618A patent/US3898794A/en not_active Expired - Lifetime
- 1973-03-27 GB GB1475473A patent/GB1417614A/en not_active Expired
- 1973-04-02 FR FR7311817A patent/FR2179019B1/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2179019B1 (en) | 1976-01-30 |
US3898794A (en) | 1975-08-12 |
FR2179019A1 (en) | 1973-11-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
746 | Register noted 'licences of right' (sect. 46/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |